Reference Command Tracking for a Linearized Model of an Air-breathing Hypersonic Vehicle

The focus of this paper is on control design and simulation for an air-breathing hypersonic vehicle. The challenges for control design in this class of vehicles lie in the inherent coupling between the propulsion system, and the airframe dynamics, and the presence of strong exibilit y eects. Working from a highly nonlinear, dynamically-coupled simulation model, control designs are presented for velocity, angle-of-attack, and altitude command input tracking for a linearized version of a generic air-breathing hypersonic vehicle model linearized about a specic trim condition. Control inputs for this study include elevator deection, total temperature change across the combustor, and the diuser area ratio. Two control design methods are presented, both using linear quadratic techniques with integral augmentation, and are implemented in tracking control studies. The rst approach focuses on setpoint tracking control, whereas in the second, a regulator design approach is taken. The eectiv eness of each control design is demonstrated in simulation on the full nonlinear model of the generic vehicle.

[1]  David K. Schmidt,et al.  Integrated control of hypersonic vehicles - A necessity not just a possibility , 1993 .

[2]  B MolerCleve,et al.  Solution of the Sylvester matrix equation AXBT + CXDT = E , 1992 .

[3]  David B. Doman,et al.  Dynamic Inversion-Based Adaptive/Reconfigurable Control of the X-33 on Ascent , 2002 .

[4]  Michael A. Bolender,et al.  A Non-Linear Model for the Longitudinal Dynamics of a Hypersonic Air-breathing Vehicle , 2005 .

[5]  Frank L. Lewis,et al.  Aircraft Control and Simulation , 1992 .

[6]  Yuri B. Shtessel,et al.  Ramjet-Powered Reusable Launch Vehicle Control by Sliding Modes , 1998 .

[7]  E. Davison,et al.  Robust control of a general servomechanism problem: The servo compensator , 1975, Autom..

[8]  David K. Schmidt Dynamics and control of hypersonic aeropropulsive/aeroelastic vehicles , 1992 .

[9]  Petros A. Ioannou,et al.  Adaptive Sliding Mode Control Design fo ra Hypersonic Flight Vehicle , 2004 .

[10]  Alan J. Laub,et al.  Solution of the Sylvester matrix equation AXBT + CXDT = E , 1992, TOMS.

[11]  Robert F. Stengel,et al.  Robust Nonlinear Control of a Hypersonic Aircraft , 1999 .

[12]  David K. Schmidt,et al.  Flight dynamics and feedback guidance issues for hypersonic airbreathing vehicles , 1999 .

[13]  Duane McRuer,et al.  Design and Modeling Issues for Integrated Airframe/Propulsion Control of Hypersonic Flight Vehicles , 1991, 1991 American Control Conference.

[14]  Frank L. Lewis,et al.  Optimal Control , 1986 .

[15]  David K. Schmidt,et al.  Uncertainty Modeling for Multivariable-Control Robustness Analysis of Elastic High-Speed Vehicles , 1999 .

[16]  David K. Schmidt,et al.  Integrated Development of the Equations of Motion for Elastic Hypersonic Flight Vehicles , 1995 .

[17]  Christopher I. Marrison,et al.  Design of Robust Control Systems for a Hypersonic Aircraft , 1998 .

[18]  David K. Schmidt Optimum Mission Performance and Multivariable Flight Guidance for Airbreathing Launch Vehicles , 1997 .

[19]  David B. Doman,et al.  Dynamic inversion-based adaptive/reconfigurable control of the X-33 on ascent , 2001, 2001 IEEE Aerospace Conference Proceedings (Cat. No.01TH8542).

[20]  David M. Bose,et al.  Flight Control Laws for NASA''s Hyper-X Research Vehicle , 1999 .

[21]  David K. Schmidt,et al.  Analytical aeropropulsive-aeroelastic hypersonic-vehicle model with dynamic analysis , 1994 .